Claims
- 1. A low vulnerability propellant having improved performance and flammability characteristics comprising a binder, cyclotetramethylene tetranitramine oxidizer, and from about 2.5 to about 15 weight percent of triaminoguanidinium salt of phosphoric acid.
- 2. A propellant of claim 1 wherein said triaminoguanidinium salt of phosphoric acid is from about 5 to about 10 weight percent of said propellant.
- 3. The propellant of claim 1 wherein said propellant is a gun propellant.
- 4. The propellant of claim 1 wherein said propellant is a rocket propellant.
- 5. The propellant of claim 1 wherein said binder is a copolymer of ethylene oxide and propylene oxide.
- 6. A method of improving the performance and flammability characteristics of low vulnerability propellants, comprising adding thereto from about 2.5 to about 15 weight percent of a triaminoguanidinium salt of phosphoric acid selected from the group consisting of traminoguanidinium diacid phosphate, bis-triaminoguanidinium monoacid phosphate, and tris-triaminoguanidinium phosphate.
- 7. The method of claim 6 wherein the amount of said triaminoguanidinium salt of phosphoric acid added is from about 5 to about 10 weight percent of said propellant.
Parent Case Info
This is a division of application Ser. No. 389,742, filed June 18, 1982, now abandoned.
US Referenced Citations (8)
Non-Patent Literature Citations (1)
Entry |
Keim et al., J. Am. Chem. Soc., 72, 4944-4946 (1950). |
Divisions (1)
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Number |
Date |
Country |
Parent |
389742 |
Jun 1982 |
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